RU2015140275A - Гибридный многослойный композиционный материал с керамической матрицей - Google Patents

Гибридный многослойный композиционный материал с керамической матрицей Download PDF

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RU2015140275A
RU2015140275A RU2015140275A RU2015140275A RU2015140275A RU 2015140275 A RU2015140275 A RU 2015140275A RU 2015140275 A RU2015140275 A RU 2015140275A RU 2015140275 A RU2015140275 A RU 2015140275A RU 2015140275 A RU2015140275 A RU 2015140275A
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facing sheet
sheet
composite material
cmc
ceramic matrix
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RU2015140275A
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RU2698695C2 (ru
RU2015140275A3 (ru
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Уильям П. КИТ
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Зе Боинг Компани
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    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71—Ceramic products containing macroscopic reinforcing agents
    • C04B35/74—Ceramic products containing macroscopic reinforcing agents containing shaped metallic materials
    • C04B35/76—Fibres, filaments, whiskers, platelets, or the like
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    • B32—LAYERED PRODUCTS
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    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
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    • C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
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  • Ceramic Engineering (AREA)
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Claims (28)

1. Гибридный многослойный композиционный материал (CMC) (10) с керамической матрицей, содержащий:
первый облицовочный лист (14), содержащий нити (22) в керамической матрице (24);
второй облицовочный лист (16), содержащий нити (22) в керамической матрице (24); и
сердцевину (12), расположенную между первым облицовочным листом и вторым облицовочным листом и скрепленную с ними посредством связующего,
причем гибридный многослойный композиционный материал CMC выполнен для воздействия на него температурным градиентом, в котором первый облицовочный лист подвержен воздействию среды с более высокой температурой, чем второй облицовочный лист,
первый облицовочный лист и второй облицовочный лист имеют по меньшей мере близко подобранные коэффициенты термического расширения, и
первый облицовочный лист имеет более высокий предел прочности при сжатии, чем второй облицовочный лист.
2. Гибридный многослойный композиционный материал CMC (10) по п. 1, в котором второй облицовочный лист (16) имеет более высокий предел прочности при растяжении, чем первый облицовочный лист (14).
3. Гибридный многослойный композиционный материал CMC (10) по п. 2, в котором
первый облицовочный лист (14) имеет предел прочности при сжатии примерно в полтора раза выше, чем предел прочности при растяжении первого облицовочного листа, и
второй облицовочный лист (16) имеет предел прочности при растяжении примерно в полтора раза выше, чем предел прочности при сжатии второго облицовочного листа.
4. Гибридный многослойный композиционный материал CMC (10) по п. 1, в котором
нити (22) первого облицовочного листа (14) и нити (22) второго облицовочного листа (16) имеют одинаковый химический состав,
причем керамическая матрица (24) первого облицовочного листа и керамическая матрица второго облицовочного листа имеют одинаковый химический состав, и
объемное содержание нитей в первом облицовочном листе равно объемному содержанию нитей во втором облицовочном листе.
5. Гибридный многослойный композиционный материал CMC (10) по п. 1, имеющий цилиндрическую форму.
6. Гибридный многослойный композиционный материал CMC (10) по п. 1, в котором диаметр нитей (22) в первом облицовочном листе (14) больше, чем диаметр нитей во втором облицовочном листе (16).
7. Гибридный многослойный композиционный материал CMC (10) по п. 1, в котором первый облицовочный лист (14) является более ортотропным, чем второй облицовочный лист (16).
8. Гибридный многослойный композиционный материал CMC (10) по п. 1, в котором предел прочности на границе между нитями (22) и керамической матрицей (24) первого облицовочного листа (14) выше, чем предел прочности на границе между нитями (22) и керамической матрицей (24) второго облицовочного листа (16).
9. Гибридный многослойный композиционный материал CMC (10) по любому из пп. 1-8, являющийся частью компонента системы (34) выпуска отработавших газов летательного аппарата,
причем первый облицовочный лист (14) облицовывает траекторию (42) движения потока отработавшего газа системы выпуска отработавших газов летательного аппарата.
10. Способ производства гибридного многослойного композиционного материала (CMC) (10) с керамической матрицей, включающий:
укладку (54) на инструментальное приспособление первого облицовочного листа (14), содержащего предварительно пропитанные спои нитей (22) в керамической матрице (24);
укладку (56) сердцевины (12) на первый облицовочный лист;
укладку (58) второго облицовочного листа (16) на сердцевину для создания стопы уложенных слоев, при этом второй облицовочный лист (16) содержит предварительно пропитанные слои нитей (22) в керамической матрице (24),
а первый облицовочный лист и второй облицовочный лист отличаются по меньшей мере одним из следующего: диаметр нитей, химический состав нитей, степень ортотропии и прочность на границе между нитями и керамической матрицей;
отверждение (60) стопы уложенных слоев при первой температуре и
спекание (62) стопы уложенных слоев при второй температуре для создания гибридного многослойного композиционного материала CMC.
RU2015140275A 2015-01-09 2015-09-22 Гибридный многослойный композиционный материал с керамической матрицей RU2698695C2 (ru)

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